{"id":38792,"date":"2017-06-05T22:23:34","date_gmt":"2017-06-05T14:23:34","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/glsv-mark-iii-rocket-conducts-all-up-launch-with-gsat-19-satellite\/"},"modified":"2017-06-05T22:23:34","modified_gmt":"2017-06-05T14:23:34","slug":"glsv-mark-iii-rocket-conducts-all-up-launch-with-gsat-19-satellite","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/glsv-mark-iii-rocket-conducts-all-up-launch-with-gsat-19-satellite\/","title":{"rendered":"GLSV Mark III rocket conducts \u2018all-up\u2019 launch with GSAT-19 satellite"},"content":{"rendered":"<p>India\u2019s GSLV Mark III rocket successfully made its first all-up launch and first attempt to reach orbit Monday in a late afternoon liftoff from the Satish Dhawan Space Centre. The launch was on schedule at 17:28 local time (11:58 UTC), with the mission tasked with lofting the GSAT-19 satellite.<\/p>\n<p>GSLV Launch:<\/p>\n<p>The first orbital launch of India\u2019s Geosynchronous Satellite Launch Vehicle Mark III (GSLV Mk.III) marked a milestone in India\u2019s space program, with the more powerful rocket allowing the Indian Space Research Organisation (ISRO) to begin launching heavier payloads aboard its own vehicles \u2013 both for spaceflight applications such as communications and in support of the country\u2019s nascent manned space program.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-medium wp-image-50669\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-024933-350x300.jpg\" alt=\"\" width=\"350\" height=\"300\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-024933-350x300.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-024933-408x350.jpg 408w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-024933.jpg 498w\" sizes=\"(max-width: 350px) 100vw, 350px\">Monday\u2019s launch came two and a half years after the GSLV Mark III\u2019s maiden flight, a successful suborbital test for which only the rocket\u2019s lower stages were live. The test flight, conducted on 18 December 2014, carried a prototype crew capsule and also served to validate the rocket\u2019s design and demonstrate the stage performance and operation of the rocket\u2019s solid-fuel first stage and liquid-fuelled second stage.<\/p>\n<p>As a result of the test flight, ISRO has refined the GSLV Mk.III\u2019s design. The nose cones of the vehicle\u2019s two large solid rocket motors now taper towards the core and the rocket will fly with an ogive-shaped payload fairing instead of the more cylindrical fairing that was used on the 2014 launch.<\/p>\n<p>GSLV Mk.III, which ISRO has also previously referred to as LVM3 \u2013 although that name now seems to have been phased out \u2013 marks the beginning of a third generation of rockets for India\u2019s orbital launch capabilities.<\/p>\n<p>India made its first orbital launch in July 1980, with a four-stage Satellite Launch Vehicle (SLV) rocket orbiting the Rohini, or RS-1, satellite. This was India\u2019s second launch attempt \u2013 a previous launch in August 1979 failed after the thrust vectoring system on the second stage malfunctioned. Following the RS-1 launch, SLV made two further launches, with one failure and one success.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>UPDATES GSLV Mk3\/GSAT-19<\/li>\n<li>65 Launch Vehicle Manuals (L2)<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>The SLV was a small vehicle, with a relatively low payload capacity of around 40 kilograms (90 lb). In order to allow heavier payloads to be launched, ISRO developed the SLV into the five-stage Augmented Satellite Launch Vehicle (ASLV). This added two solid rocket motors \u2013 based on the SLV\u2019s first stage \u2013 to the sides of the rocket, burning as the first stage of the new vehicle. The modified SLV served as the second to fifth stages of the ASLV.<\/p>\n<p>In four launches between March 1987 and May 1994, the ASLV achieved two failures, one partial failure and completed one mission successfully.<\/p>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>Instead of continuing to invest in the ASLV, India opted to develop a new generation of larger rockets. The new Polar Satellite Launch Vehicle (PSLV) first flew in September 1993. Despite the failure of its maiden flight, and a partial failure on its first operational launch four years later, the PSLV has become the workhorse of India\u2019s space program. It has made thirty-nine launches to date, including the deployments of the Chandrayaan 1 lunar probe and the Mars Orbiter Mission.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-50670\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025353-350x223.jpg\" alt=\"\" width=\"350\" height=\"223\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025353-350x223.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025353-549x350.jpg 549w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025353.jpg 615w\" sizes=\"(max-width: 350px) 100vw, 350px\">The PSLV forms the basis for ISRO\u2019s Geosynchronous Satellite Launch Vehicle, in its Mark I and Mark II configurations. GSLV replaces the PSLV\u2019s solid rocket boosters with larger liquid boosters, and the PSLV\u2019s third and fourth stages with a single cryogenic upper stage. The Mark I GSLV used a stage developed between India and Russia, powered by a Russian KVD-1M engine. The Mark II vehicle replaced this with an all-Indian stage and engine.<\/p>\n<p>First flown in April 2001, the GSLV initially struggled for reliability. The rocket\u2019s maiden flight failed, although the second and third launches successfully deployed their payloads. Beginning with its fourth launch, in July 2006, the rocket entered a run of four consecutive launches without success \u2013 with one delivering its payload to a lower-than-planned orbit and three falling short of orbit altogether. Since January 2014 the GSLV Mk.II has posted four consecutive successful launches.<\/p>\n<p>Despite sharing a name with its predecessors, the GSLV Mk.III is a completely new vehicle to the Mk.I and Mk.II. The Mark III is a three-stage rocket, with a first stage comprised of two solid rocket motors mounted on either side of a liquid-fuelled core, containing two stages.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-50668\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023546-350x267.jpg\" alt=\"\" width=\"350\" height=\"267\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023546-350x267.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023546-458x350.jpg 458w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023546-768x587.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023546.jpg 783w\" sizes=\"(max-width: 350px) 100vw, 350px\">GSLV Mark III launches take place from the Second Launch Pad (SLP) at the Satish Dhawan Space Centre \u2013 a launch complex which is shared with the PSLV and the GSLV Mark II. In preparation for Monday\u2019s launch the rocket, designated GSLV Mk.III D1, was stacked atop a mobile launch pedestal in the complex\u2019s Vehicle Assembly Building. The assembled rocket was then rolled out to the launch pad a few days in advance of liftoff.<\/p>\n<p>The Second Launch Pad, along with the nearby First Launch Pad (FLP) have been used for all of India\u2019s orbital launches since the ASLV was retired. SLV and ASLV launches took place from older pads, to the South of the active launch complexes. The First Launch Pad is used mostly for PSLV launches. Since the Second Launch Pad was completed in 2005, it has been used for all GSLV launches.<\/p>\n<p>Monday\u2019s launch was the twenty-first from the Second pad.<\/p>\n<p>The Satish Dhawan Space Centre is named after former ISRO chairman Satish Dhawan. Prior to Dhawan\u2019s death in 2002, the facility was named the Sriharikota High Altitude Range (SHAR). The launch site \u2013 located on the island of Sriharikota on India\u2019s east coast, just north of Chennai \u2013 has been used for all of India\u2019s orbital launches.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-50671\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025446-350x248.jpg\" alt=\"\" width=\"350\" height=\"248\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025446-350x248.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025446-494x350.jpg 494w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-025446.jpg 598w\" sizes=\"(max-width: 350px) 100vw, 350px\">The two S200 motors that make up GSLV Mk.III\u2019s first stage are 26.2 meters (86.0 feet) long with a diameter of 3.2 meters (10 feet).<\/p>\n<p>Each S200 contains 205 tons (202 imperial tons, 226 US tons) of solid propellant, which is composed of ammonium perchlorate, aluminum and hydroxyl-terminated polybutadiene (HTPB).<\/p>\n<p>First stage ignition occurred at liftoff, beginning a 140-second burn. After lifting off, GSLV flew downrange along an azimuth of 107 degrees.<\/p>\n<p>About 114 seconds after liftoff, the rocket\u2019s second stage \u2013 the lower stage of the core vehicle \u2013 ignited. This is an L110, powered by a pair of Vikas engines. The Vikas is a license-built version of the French Viking rocket engine, which powered Europe\u2019s Ariane 1, 2, 3 and 4 rockets between 1979 and 2004.<\/p>\n<p>India has previously used Vikas aboard PSLV and GSLV rockets. The second stage burns unsymmetrical dimethylhydrazine (UDMH) propellant, oxidized by dinitrogen tetroxide. First stage burnout and separation occurred twenty-six seconds after second stage ignition.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-50667\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023414-350x229.jpg\" alt=\"\" width=\"350\" height=\"229\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023414-350x229.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023414-536x350.jpg 536w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023414.jpg 654w\" sizes=\"(max-width: 350px) 100vw, 350px\">At staging, GSLV Mk.III D1 was at an altitude of around 62 kilometers (39 miles, 33 nautical miles), traveling downrange at a speed of 1.95 kilometers per second (4,360 mph). At around three minutes and 45 seconds mission elapsed time, with the rocket at an altitude of about 116 kilometers (72 miles, 63 nautical miles), the payload fairing separated from around GSAT-19 at the nose of the rocket.<\/p>\n<p>The second stage burned for three minutes and twenty-three seconds, shutting down five minutes and 17 seconds after liftoff. The spent stage was jettisoned three seconds later, with third stage ignition two seconds after separation. This began a ten-minute, 43-second burn for the C25 second stage. Powered by an Indian CE20 cryogenic rocket engine, the C25 burns liquid hydrogen oxidized by liquid oxygen.<\/p>\n<p>When the third stage shut down sixteen minutes and five seconds after liftoff, GSLV Mk.III D1 was in a geosynchronous transfer orbit with a perigee of 170 kilometers (106 miles, 91.8 nautical miles), an apogee of 35,975 kilometers (22,354 miles, 19,425 nautical miles) and inclination of 21.5 degrees. GSAT-19 will separate from the rocket fifteen seconds after cutoff.<\/p>\n<p>The 3,136-kilogram (6,914 lb) GSAT-19 is the heaviest satellite India has ever launched, to any orbit, using its own rockets. More than half of the satellite\u2019s mass is propellant, much of which will be expended during initial orbit-raising, when the satellite will maneuver from its initial transfer orbit into an operational geostationary orbit. A liquid apogee motor, generating 440 Newtons (99 pounds-force) of thrust, will be used for this purpose. The satellite has a dry mass of 1,394 kilograms (3,073 lb).<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-50666\" src=\"\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346-350x233.jpg\" alt=\"\" width=\"350\" height=\"233\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346-350x233.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346-525x350.jpg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346-585x390.jpg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346-263x175.jpg 263w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2017\/06\/2017-06-05-023346.jpg 639w\" sizes=\"(max-width: 350px) 100vw, 350px\">GSAT-19 was built by ISRO and is based on the three-axis-stabilised I-3K satellite bus. It carries four Ku\/Ka band forward link transponders and four return link transponders.<\/p>\n<p>The spacecraft\u2019s mission is primarily technology demonstration, serving to test new systems in geostationary orbit for use on future Indian communications satellites. Technologies to be tested include more miniaturized forms of heat pipe intended to provide better thermal control, micro electromechanical (MEMS) accelerometers and fiber optic gyroscopes to help determine the attitude of the satellite.<\/p>\n<p>Also aboard GSAT-19 is the Geostationary Radiation Spectrometer (GRASP), which will detect and study charged particles in the satellite\u2019s environment. This will help to characterize the effect of these particles on the satellite and its electrical systems. GSAT-19 will initially be stationed at a longitude of 74 degrees East.<\/p>\n<p>The GSAT-19 spacecraft has a design life of ten years. The satellite is powered by a pair of solar arrays capable of generating 4.5 kilowatts of electrical power, and is also equipped with an Indian-manufactured lithium-ion battery which can store 100 amp-hours of energy for subsequent use.<\/p>\n<p>Monday\u2019s launch was the third of the year for India, following a PSLV launch in February which deployed the Cartosat-2D military imaging satellite along with 103 other spacecraft, and May\u2019s GSLV Mk.II flight with the GSAT-9 satellite aboard. India\u2019s next launch is expected around the end of this month, with a PSLV carrying another Cartosat spacecraft into orbit. The GSLV Mk.III\u2019s next launch will carry India\u2019s GSAT-20 communications satellite \u2013 this is currently scheduled for no earlier than December, or more likely early 2018.<\/p>\n<p>(Images via ISRO).<\/p>\n","protected":false},"excerpt":{"rendered":"<p>India\u2019s GSLV Mark III rocket successfully made its first all-up launch and first attempt to reach orbit Monday in a late afternoon liftoff from the Satish Dhawan Space Centre. The launch was on schedule at 17:28 local time (11:58 UTC), with the mission tasked with lofting the GSAT-19 satellite. GSLV Launch: The first orbital launch [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[1259,525],"class_list":["post-38792","post","type-post","status-publish","format-standard","hentry","category-news","tag-gslv","tag-isro"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38792"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=38792"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/38792\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=38792"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=38792"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=38792"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}